On-Orbit Thermal Analysis of Ring Truss-Type Deployable Antenna

Author:

Zhang Xiong,Kang Xi,Huang Hailin,Li Bing

Publisher

Springer Nature Singapore

Reference18 articles.

1. He P (2016) Analysis and control of thermally induced vibration for on-orbit satellite antenna. Dalian University of Technology, Dalian

2. Gunnar T (2022) Deployable tensegrity structures for space applications. Doctoral thesis of the Royal Institute of Technology, Department of Mechanics, UK

3. Semler D, Tulintseff A, Sorrell R et al (2010) Design, integration, and deployment of the TerreStar 18-meter reflector. In: 28th AIAA international communications satellite systems conference. AIAA, p 8855

4. Medzmariashvili E, Tserodze S, Tsignadze N et al (2006) A new design variant of the large deployable space reflector. In: The 10th biennial international conference on engineering, construction and operations in challenging environments. ASCE, pp 1–8

5. Tian DK (2011) Design and experimental research on truss structure for modular space deployable antenna. Harbin Institute of Technology, Harbin

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